Wind turbine blade having a root region with elongated fastening members provided with metal fibres

ABSTRACT

A wind turbine blade for a wind turbine is a shell structure of a fibre-reinforced composite and comprises a root region and an airfoil region. The root region has ring-shaped cross section and comprises a plurality of elongated bushings  7  with an inner thread  22  and embedded interspaced in the fibre-reinforced polymer so as to substantially follow the circumference of the root region and allow access from the outside to the inner threads. Each fastening member  7  is provided with a notch  60′  in the periphery  11  thereof. A rod-shaped locking element  61  passes through the notch  60′  in engagement therewith. The locking element  61  is fixedly and tightly fitting arranged in a through-going circular bore  65  extending through the wall of the root region.

TECHNICAL FIELD

The present invention relates to a wind turbine blade for a wind turbinerotor comprising a hub from which the wind turbine blade extends whenmounted to the hub, the wind turbine blade including a shell structureof a fibre-reinforced composite material comprising fibres embedded in apolymer matrix, the wind turbine blade extending in longitudinaldirection and having a profiled contour including a pressure side and asuction side as well as a leading edge and a trailing edge, said edgesdefining a chord plane therebetween, when seen in the longitudinaldirection the profiled contour comprising a root region with a root endface, an airfoil region and optionally a transition region between theroot region and the airfoil region, the root region having a ring-shapedcross section with an outer surface and an inner surface, the rootregion comprising a plurality of elongated fastening members providedwith fastening means and embedded mutually spaced apart in thefibre-reinforced polymer so as to substantially follow a circumferenceof the root region and allow access from the outside to the fasteningmeans used for mounting the blade to the hub, the fastening memberscomprising a first end arranged at the root end face, a second endopposite the first end thereof, an outer surface, an inner surface, afirst lateral face and an opposite second lateral face.

BACKGROUND ART

Wind turbine blades and thereby also the root region thereof are oftenmade by assembling two blade halves essentially corresponding to thesuction side and the pressure side, respectively, along the chord plane.However, the blades may also be moulded in their entirety by so-calledhollow moulding.

The root region comprises layers of fibres forming an outer layer and aninner layer between which fastening members in the form of bushings areplaced. A separately formed inserts may be placed between each pair ofadjacent bushings, whereby the bushings are mutually separated by theinserts. The known inserts are made of glass fibres embedded in asuitable resin.

A potential problem in connection with wind turbine blades is loadtransfer from the fibre composite structure of the root region to thehub of the wind turbine. The connection and transfer of loads from theblade to the hub is inter alia provided by mounting the blade to the hubby screwing bolts into the bushings placed in the root or by means ofnuts screwed onto stud bolts screwed into the bushings. In case thenumber of bolts and thereby the number of bushings has to be increasedto handle a given load, remaining area of the fibre composite materialbetween the bushings is reduced. This may result in the root connectionbeing insufficiently supported to withstand the loads, whereby theconnection between the blade root and the hub may fail since thebushings are insufficiently retained in the composite material and thuspulled out of the composite material of the root region. This isespecially a problem when long and thereby heavy blades are to be used.

WO 2010/018225 provides a method of manufacturing a wind turbine bladecomprising a steel wire or steel fibre-reinforced polymer matrix.However, the document does not address the problem of how the rootregion is to be designed to withstand extreme loads in the connectionbetween the blade root and the hub.

EP 2 138 716 describes a blade insert provided in the lamination of awind turbine blade. The insert is made up of two parts, namely a headand a body. The head is designed so as to be able to screw the insertonto another structure. The body has a cylindrical exterior and has aconical cavity. Thereby, the body provides a smooth transition to theblade laminate.

DE 196 25 426 discloses a rock anchor comprising a core element made ofpolymer and provided with outer threads. The outer part of the rockanchor is reinforced with glass fibres. The anchor is particularlysuited for non-conductive, non-magnetic and dielectric parts.

EP 1 463 625 discloses a method of manufacturing root end bushings withwedges provided in extension of the bushings.

DISCLOSURE OF THE INVENTION

It is an object of the invention to provide a wind turbine blade with aroot region overcoming at least one of the drawbacks of the prior art orat least provides a useful alternative.

According to a first aspect of the invention, a wind turbine blade ofthe type described is provided with a root region, wherein at least oneof the elongated fastening members comprises metal fibres, a first endthereof being firmly fixed to the fastening member and the remainingportion thereof extending outwardly from the fastening member and beingembedded in the polymer matrix of the fibre-reinforced compositematerial.

The metal fibres firmly fixed to the fastening member and embedded inthe polymer matrix of the composite material provides an improvedretention of the fastening member, as both the fastening member and themetal fibres firmly fixed thereto are retained in the polymer matrix. Asa result, the blades are reliably secured to the hub of the windturbine. Due to the improved retention of the fastening members, itpossible to attach longer and thereby heavier blades to the hub withoutincreasing the diameter of the root region and/or the number offastening members. Further, the metal fibres, advantageously steelfibres, have material properties that are compatible with the fasteningmeans, since these are typically made of metal and often steel.

Further, due to use of metal fibres the manufacturing time of a blade orblade halves may be reduced compared to conventional methods, whereinmetal fibres are not used, such as forming the blade or blade halves bymeans of pre-impregnated fibres or by means vacuum assisted resintransfer moulding, VARTM. This is especially due to the properties ofthe surface of metal fibres compared to the conventional fibres, such asglass fibres. Finally, metal is a better heat conductor than glassfibres, whereby the curing process may be improved.

According to an embodiment of the invention the outwardly extendingportion of the fibres may end in a second fibre end.

It is preferred that the metal fibres have an outer free second end.However, it should be noted that it is also possible to firmly fix boththe first and the second fibre end to the fastening member so that themetal fibres form a loop being embedded in the polymer matrix of thefibre-reinforced composite material.

According to another embodiment the metal fibres are firmly fixed to thesecond end of the fastening member.

According to a further embodiment of the invention the above metalfibres may be firmly fixed to an outer surface of the fastening member.

The metal fibres may be firmly fixed to the fastening member by casting,gluing, soldering or brazing.

The choice of method depends on the material of the elongated fasteningmember and the metal fibres.

It should be noted that the first fibre end also may firmly fixed to thefastening member by mechanical means. As an example, the first end ofthe metal fibres may be firmly clamped between portions of the fasteningmembers, such as in a compressed opening in the fastening member.

According to a further embodiment of the invention at least 50, 60, 70,80, 90 or 100% of the fastening members may be provided with firmlyfixed metal fibres.

It is preferred that all of the fastening members are provided withfirmly fixed metal fibres so that the retention of all of the fasteningmembers is improved and an optimum connection between the blade the hubis obtained.

According to yet another embodiment, the metal fibres may have anE-modulus being at least twice and preferably thrice the E-modulus ofglass fibres, the metal fibres preferably being steel fibres.

As a result, a suitable retention of the fastening members is obtained.

According to a further embodiment, the metal fibres may have a crosssection in a range between 0.04 mm and 1.0 mm or in a range between 0.07and 0.75 mm or in a range 0.1 and 0.5 mm.

According to another embodiment, the metal fibres may be fixed to thefastening member as a bundle of fibres.

In this embodiment the fixation of the metal fibres to the fasteningmembers is facilitated as compared to fixing the fibres separately tothe fastening members.

Additionally, the metal fibres may extend from the fastening members insuch manner that they are arranged in at least one separate layer of thefibre-reinforced composite material.

One or more layers comprising metal fibres may be arranged up to thelayer comprising metal fibres. The layer may comprise metal fibres orfibres different from metal fibres, e.g. be without metal fibres.

The at least one separate layer comprising metal fibres may comprise 20,30, 40, 50, 60, 70, 80, 90 or 100% by volume of metal fibres, theremaining fibres being a different type of fibres than metal fibres,preferably glass and/or carbon fibres.

The metal fibres may extend outwardly from the fastening members in amutually diverging manner.

The metal fibres may extend from the fastening members in a fan-shapedmanner so as to be arranged in a common plane. Optionally, the metalfibres may extend from the fastening members in a cone-shaped manner.

According to another embodiment, the fastening members may be bushingspreferably having a uniform cross section and the fastening means may bea thread in a bore in the bushing.

The fastening member may, however, also be a rod preferably having auniform cross section and the fastening means may be an outer thread ofthe rod.

The fastening members may preferably be made of metal, preferably steel.

Further, the fastening members and the metal fibres firmly fixed theretomay be made of the same material or compatible materials.

Thereby, the fixation of the fibres to the fastening members isfacilitated.

According to a further embodiment, the root region may compriseintermediate retaining means comprising metal fibres, preferably steelfibres, and arranged in the regions between adjacent interspaced lateralsurfaces of the fastening members, preferably in each region betweenadjacent fastening members, and preferably extending at least from thefirst to the second end of the fastening members when seen in thelongitudinal direction of the blade.

The intermediate retaining means may comprise a number of first layerscomprising metal fibres and preferably also a number of intermediatesecond layers comprising a different type of fibres than metal fibres,preferably glass and/or carbon fibres.

The intermediate retaining means may advantageously be formed asseparate inserts embedded in the polymer matrix, said inserts comprisinga first insert part substantially corresponding to the region betweenthe lateral faces of adjacent fastening members.

By using intermediate retaining means comprising metal fibres, therigidity of the root region is improved, thereby also improving theretention of the fastening members.

The polymer of the fibre-reinforced composite material may be epoxy,polyester, vinylester or any suitable polymer and in addition to metalfibres the fibres of the fibre-reinforced composite material arepreferably carbon and/or glass fibres.

The outer surface of the fastening members may be corrugated, wherebythe surface area of the fastening members is increased and provides anenhanced retention of the fastening members in the surrounding polymermatrix.

The phrase “metal fibres” also covers metal filaments and metal wires.

Further, the metal fibres may be coated with another metal in order toimprove the adherence to the polymer matrix. As an example, steel fibresmay be coated be with zinc or brass.

Additionally, the metal fibres may be incorporated into mats or stripscomprising fibres, which may be chopped fibres, or arrangedunidirectionally or multi-directionally.

Advantageously, the fastening members (or the bushing) are bonded intothe composite material of the root region. More advantageously, thefastening members are laminated into the composite material of the rootregion.

The majority of the blade may be reinforced with fibres of another type,typically glass fibres or carbon fibres. In particular the profiledregion of the blade having an airfoil profile and the transition regionmay be reinforced by such fibres. Thereby only the root region andoptionally only the region, wherein the bushings are laminated into thecomposite structure, may be reinforced by metal fibres, advantageouslybeing steel fibres.

According to a second aspect, the invention provides an embeddingelement for embedment in the root of a wind turbine blade of afibre-reinforced composite material is elongated and has a first end andan opposite second end, a first longitudinal lateral face and anopposite second longitudinal lateral face, an upper face and a lowerface interconnecting the lateral faces, the embedding element is formedof a fibre-reinforced composite material comprising fibres embedded in apolymer matrix and comprises an elongated fastening element of metalhaving an outer surface, a first end and an opposite second end, and afastening means accessible from the first end, said fastening elementbeing embedded in the fibre-reinforced composite material, said firstend of the fastening element being arranged at the first end of theembedding element, wherein a fastening element of an embedding elementof the above described type is provided with metal fibres, a first endthereof being firmly fixed to the fastening element and remainingportion thereof extending outwardly from the fastening element and beingembedded in the fibre-reinforced polymer matrix of the embeddingelement.

The adherence of the metal fibres to the polymer matrix and the firmfixation of the metal fibres to the fastening element provide for animproved retention of the fastening element in the embedding element.Additionally, the metal fibres improve the rigidity of the embeddingelement. As a result, the embedding element provides for an increasedstrength of the retention of the embedding element in the blade andthereby an improvement of the strength of the fixation of the blade tothe hub of the wind turbine.

The fastening element may be embedded in the fibre-reinforced compositematerial of the embedding element, except for the first end of thefastening element being arranged at the first end of the embeddingelement.

The polymer matrix may be a resin such a polyester, epoxy or vinylester,however, any appropriate polymer can be used.

The fibres of the fibre-reinforced composite material may be anyappropriate fibres, however, at present glass fibres and/or carbonfibres and/or metal fibres, especially steel or iron fibres, arepreferred.

The fibre-reinforced composite material of the wind turbine blade and/orthe root thereof may comprise the same polymer and fibres as mentionedabove for the fibre-reinforced composite material of the embeddingelement.

According to an embodiment, the outwardly extending portion of the metalfibres ends in a second fibre end.

It is preferred that the metal fibres have an outer free second end.However, it should be noted that it is also possible to firmly fix boththe first and the second fibre end to the fastening element so that themetal fibres form a loop being embedded in the polymer matrix of thefibre-reinforced composite material of the embedding element.

According to a further embodiment, the metal fibres are firmly fixed tothe second end of the fastening element.

According to a further embodiment, the metal fibres are firmly fixed tothe outer surface of the fastening element.

The metal fibres may be firmly fixed to fastening element by casting,gluing, soldering or brazing.

The choice of the method for firmly fixing the fibres to the fasteningelements depends on the material of the elongated fastening element andthe metal fibres.

It should be noted that the metal fibres may also be firmly fixed to thefastening element by mechanical means. As an example, the first end ofthe metal fibres may be firmly clamped between portions of the fasteningelement such as in a compressed opening in the fastening element.

According to a further embodiment, the metal fibres have an E-modulusbeing at least twice and preferably thrice the E-modulus of glassfibres.

According to an additional embodiment, wherein the metal fibres have across-section in the range between 0.04 mm and 1.0 mm or in a rangebetween 0.07 mm and 0.75 mm or in a range between 0.1 mm and 0.5 mm.

The metal fibres may be fixed to the fastening elements as single fibresor as one or more bundle(s). The use of one or more bundles of fibres ispreferred.

According to a further embodiment, the fibres are iron or steel fibres.

In a further embodiment, the elongated fastening element has asubstantially uniform cross-section between the first and the second endthereof.

The elongated fastening element may have a substantially circularcross-section, whereby the manufacturing thereof is facilitated.

In an addition embodiment, the fastening element has a corrugated outersurface.

The corrugated outer surface of the fastening element provides animproved adherence thereof to the polymer matrix of the fibre-reinforcedcomposite material of the em-bedding element.

The fastening means of the fastening element may be an inner thread in alongitudinal bore. According to an additional embodiment, the elongatedfastening element is made of iron or steel.

According to an embodiment, the embedding element has a substantiallyuniform cross-section over at least a portion of the length thereof.

The embedding element may have a substantially quadrangularcross-section over at least a portion of the length thereof, the upperand lower face of the embedding element being preferably substantiallyparallel over said portion or the length thereof.

The elongated element may have a substantially rectangular or trapezoidcross-section. The embedding element may, however, also have a circularcross-section.

According to a further embodiment, the embedding element tapers over atleast a portion of the length thereof. The embedding element may taperin a direction from the first end thereof towards the second endthereof, and the tapering may be gradual so as to provide a wedge-shapedembedding element.

Preferably, the upper face of the embedding elements tapers towards thelower face thereof.

According to an additional embodiment, the first longitudinal lateralface of the embedding element extends substantially convexly in across-sectional view of the embedding element, and the secondlongitudinal lateral face of the embedding element extends substantiallycorrespondingly concavely in a cross-sectional view of the embeddingelement.

Due to the concave and convex lateral surface juxtaposed embeddingelements may be rotated in relation to each other, the first lateralface of each embedding element still engaging the second lateral face ofthe juxtaposed embedding element. The first and the second lateral facemay have substantially circular convex and concave shape as see in across-sectional view. As a result thereof, it is possible to arrangejuxtaposed embedding elements so as to form various curve shapes such asa circular cross-sectional shape of the blade root. The same type ofembedding elements may thus be used for blade roots of differentdiameters.

The embedding element may be made by a method involving pultrusion, i.e.the fibre-reinforced composite material of the embedding element may beprovided by pultrusion. It should, however, be noted that thefibre-reinforced composite material may be provided by any known methodof producing products of a fibre-reinforced composite material. Inaddition to pultrusion suitable methods include dry lay up of fibrematerial which is subsequently supplied with a resin, e.g. RTM or VARTM,or lay up of pre-impregnated fibre material which is subsequently cured.

According to a third aspect, the present invention relates to a methodof producing a wind turbine blade of a fibre-reinforced compositematerial, wherein a plurality of embedding elements are such embedded injuxtaposition in the polymer matrix of the fibre-reinforced compositematerial of the wind turbine blade that they follow the circumference ofthe root region, the first lateral face of each embedding elementengaging the second lateral face of the juxtaposed embedding element andallowing access to the outside to the fastening means, which may be usedfor securing the blade to the hub of the wind turbine blade. Thefastening means of the fastening element may be an inner thread in alongitudinal bore.

Although this embodiment is a preferred embodiment, the fastening meansof the fastening element may also be an outer threaded rod-shaped partof the fastening element extending from the first end thereof.

The various aspects of the invention may be combined in any way.

BRIEF DESCRIPTION OF THE DRAWINGS

The invention is explained in greater detail below with reference to thedrawings, in which

FIG. 1 shows a wind turbine,

FIG. 2 is a diagrammatic perspective view of a wind turbine bladeaccording to the invention,

FIG. 3 is a perspective, longitudinal, sectional view of a portion of aroot region of a first embodiment of a wind turbine blade according tothe invention comprising a first embodiment of fastening membersprovided with metal fibres,

FIG. 4 shows a portion of the root region shown in FIG. 3,

FIG. 5 is a diagrammatic view of a second embodiment of an elongatedfastening member provided with metal fibres firmly fixed thereto,

FIG. 6A shows a third embodiment of an elongated fastening memberprovided with metal fibres firmly fixed thereto,

FIG. 6B shows a fourth embodiment of an elongated fastening memberprovided with metal fibres firmly fixed thereto,

FIG. 7 shows a fifth embodiment of an elongated fastening memberprovided with metal fibres firmly fixed thereto,

FIG. 8 shows a sixth embodiment of an elongated fastening memberprovided with metal fibres firmly fixed thereto,

FIG. 9 shows in an enlarged scale a detail of FIG. 3 and discloses afastening member in form of a bushing arranged next to a separatepre-made insert,

FIG. 10 is a diagrammatic perspective view of a first embodiment of anembedding element according to the invention,

FIG. 11 is a longitudinal view along the line IV-IV in FIG. 10,

FIG. 12 is a longitudinal sectional view of a blank from which twoembedded elements can be made, the blank being shown in a state where ithas been cut to provide the two embedding elements,

FIG. 13 is a schematic view of a pultrusion system for manufacturing apultruded string from which the blank shown in FIG. 12 can be cut,

FIG. 14 is a schematic view of a portion of three embedding elementsaccording to the invention arranged so that the lateral faces thereofabut each other, and

FIG. 15 is a perspective view the root of a wind turbine blade withembedding elements embedded in the root region thereof.

DETAILED DESCRIPTION OF THE INVENTION

FIG. 1 illustrates a conventional, modern upwind turbine 24 according tothe so-called “Danish concept” with a tower 36, a nacelle 25 and a rotorwith a substantially horizontal rotor shaft. The rotor includes a hub 23and three blades 2 extending radially from the hub 23, each having ablade root 31 nearest the hub, and a blade tip 32 furthest from the hub23.

As evident seen from FIG. 2, the blade 2 comprises a root region 26 witha root end face 29 closest to the hub, an airfoil region 27 furthestaway from the hub, and a transition area 28 between the root region 26and the airfoil region 27. The airfoil region 27 has an ideal or almostideal blade shape, whereas the root region 26 has a substantiallycircular cross section, which reduces storm loads and makes it easierand safer to mount the blade 2 to the hub 23. Preferably, the diameterof the blade root 31 is constant along the entire root region 26. Thetransition region 28 has a shape gradually changing from the circularshape of the root region 26 to the airfoil profile of an airfoil region27. The width of the transition region 28 increases substantiallylinearly with increasing distance from the hub 23.

The blade is often made of two blades halves assembled by being glued orbolted together substantially along a chord plane 35 of the blade. Theblade 2 comprises a leading edge 34 facing the rotational direction ofthe blade 2 when the blade 2 is mounted on the hub 23 and a trailingedge 33 facing in the opposite direction of the leading edge 34. Thechord plane 35 extends between the leading edge 34 and the trailing edge33 of the blade 2. It should be noted that the chord plane does notnecessarily run straight over its entire extent, since the blade may betwisted and/or curved, thus providing a chord plane with acorrespondingly twisted and/or curved course, this being most often thecase in order to compensate for the local velocity of the blade beingdependent on the radius from the hub. Due to the circular cross section,the root region 26 does not contribute to the production of the windturbine and, in fact, it lowers the production slightly due to the windresistance.

As seen in FIGS. 3 and 4, the blade including the root region 26 isformed as a shell structure. The shell structure of the root region 26is ring-shaped and comprises an outer surface 3 formed by an outer layer5 of a fibre-reinforced polymer matrix advantageously of glass fibresand/or carbon fibres and a resin, such as epoxy, polyester orvinylester, and an oppositely arranged inner surface 4 formed by aninner layer 6 being made of the same material as the outer layer 5.Elongated fastening members 7 with fastening means 22 are placed betweenthe layers 5, 6. Advantageously, the elongated fastening members 7 arebushings having a circular cross section and comprise a central bore 12with an inner thread 22 as fastening means. The bushing 7 comprises afirst end 9 and an oppositely arranged second end 10. The first end 9 ofthe bushing 7 is placed at the root end face 29 of the root region. Thebushings 7 are arranged mutually spaced apart so as to substantiallyfollow the circumference of the root region and allow access from theoutside to the fastening means 22, i.e. the threads used for mountingthe blade to the hub. Seen relative to the root region, the outerperiphery 11 of the fastening members 7 comprises a radially outersurface 11 a, an opposite radially inner surface 11 b, a first lateralface 11 c, and an opposite lateral face 11 d, as shown in FIG. 5.

Intermediate retaining means comprising metal fibres 13 is arranged ineach region between adjacent interspaced lateral surfaces 11 c, 11 d ofthe fastening members 7, i.e. in the present example the bushings.Further, in the present embodiment the intermediate retaining means areformed of separately manufactured inserts 39. As it appears from FIG. 9,the inserts 39 comprise a first insert part 40 and a second insert part41. The first insert part 40 essentially corresponds to the regionbetween the lateral faces 11 c, 11 d of adjacent bushings 7 and isprovided with opposite lateral faces 42, 43 formed complimentary to thelateral faces 11 c, 11 d of the adjacent bushings 7. The inserts 39substantially extend up next to the adjacent bushings when seen incircumferential direction. Further, the first insert part 40 extendsfrom the first end of the bushings 7 and beyond the second end thereof,as clearly seen in FIG. 9. The second insert part 41 is a wedge-shapedtapering extension of the first insert part 40. As seen in radialdirection of the root region, the first insert part 40 has an extentsubstantially corresponding to that of the bushings.

As seen in FIG. 9, the intermediate retaining means formed of theseparately manufactured and pre-formed insert 39 comprises a number offirst layers 16 comprising metal fibres and intermediate second layers37 comprising a second fibre material 38 differing from the metalfibres. The first layers 16 comprising metal fibres 13 may be formed ofmats comprising metal fibres. The metal fibres are preferably of amaterial having an E-modulus of at least twice, preferably thrice theE-modulus of glass fibres. A preferred material for the metal fibres issteel. The steel fibres or steel filaments may also be formed into steelwires having a cross-sectional dimension in the range between 0.04 mmand 1.0 mm, or in the range between 0.07 mm and 0.75 mm in the rangebetween 0.1 mm and 0.5 mm. The second layers 37 comprising a differenttype of fibres than metal fibres preferably comprise glass and/or carbonfibres. The layers 37 may be formed of fibre mats. During manufacture ofthe inserts 39 the layers comprising the metal fibres and the layerscomprising a second type of fibres differing from the metal fibres areembedded in a suitable resin such as polyester, epoxy or vinylester. Oneof the suitable methods for manufacturing the inserts 39 is pultrusion,whereby elongated fibre-reinforced products having a uniform crosssection may be produced.

As seen in FIG. 3, a wedge-shaped element 17 is arranged behind eachbushing 7 as seen in the longitudinal direction of the blade. A firstend 18 of the element 17 is arranged in abutment with the second end ofthe bushing 7, and a second end 19 of the element 17 is tapered. Thewedge-shaped elements 17 are made of balsawood or a hard polymer foam oranother similar material. In a longitudinal sectional view, the bushing7 and the abutting wedge-shaped element 17 have a shape corresponding tothe shape of the insert 39 so that the wall thickness of the root regiondecreases gradually in the longitudinal direction of the blade.

As shown in FIGS. 3-4, the bushings 7 are provided with metal fibres 13having a first fibre end 201 and an opposite second fibre end 202. Thefirst fibre end 201 of the metal fibres is firmly fixed to the secondend 10 of the bushing 7, especially the end face of the bushing 7. Aportion 203 of the metal fibres extends outwardly from said end face. Asmentioned, the metal fibre 13 may be fixed to the end face of thebushings 7 and/or close thereto at the outer surface 11 of the bushings7.

As shown in FIG. 4, the fibres 13 extend from the second end 10 of thebushing 7 in a fan-shaped manner so that the distance between the secondfibre ends 202 of adjacent fibres exceeds the distance between the firstends 201 of adjacent fibres. The outwardly extending portions 203 of themetal fibres 13 are embedded in the polymer matrix of thefibre-reinforced composite material of the root region. In addition tothe metal fibres 13 the fibre-reinforced composite material of the rootregion comprises additional fibres, which also may be metal fibresand/or fibres other than metal fibres such as carbon and/or glassfibres. Preferably, the metal fibres are steel fibres and may be firmlyfixed to the bushings 7 by welding, casting, gluing, soldering orbrazing depending on the considered most suitable method and furtherdepending on the material of the fibres and the bushings 7. The metalfibres may, however, also be firmly fixed to the bushings 7 bymechanical means. As an example, the first fibre end of the metal fibres13 may be firmly clamped between portions of the bushings 7 such as in acompressed opening in the bushing 7.

FIG. 5 shows a second embodiment of the bushing 7 comprising metalfibres 13 firmly fixed to the outer periphery 11 of the bushing 7. Theouter periphery of the bushing 7 is corrugated so as to increase thesurface area thereof.

FIG. 6A shows a third embodiment of a bushing 7 provided with outwardlyextending metal fibres 13. The metal fibres 13 are arranged inunidirectional fibre bundles 204. Each bundle 204 is firmly fixed to thesecond end 10 of the bushing 7. The bundle 204 is fixed to the secondend 10 in separate circular rows. A first circular row is placed nearthe periphery of the second end 10 and a second circular row is placedinwardly of the first row. The bushing 7 and the fibre bundles 204 areembedded in the polymer matrix of the fibre-reinforced compositematerial of the root region. Additional fibres, such as steel fibres orfibres of a different material than metal, are preferably placed in thearea between the bundles 204. The fibre bundles 204 are firmly fixed tothe bushings 7 as explained above.

FIG. 6B shows a fourth embodiment of a bushing 7 comprising metal fibres13. The metal fibres 13 are arranged unidirectionally and each of thefibres is separately firmly fixed to the bushing 7.

FIG. 7 shows a fifth embodiment of a bushing 7 comprising metal fibres13. The metal fibres 13 are firmly fixed to the second end 10 in bundles204 and are arranged multidirectionally. As shown, layers of a secondfibre material 38 different from metal fibres are arranged between thefibre bundles 204 extending from the second end 10 of the bushing 7 soas to substantially form a fan. However, as shown, some of the metalfibres 13 may cross and pass through the layers of the second fibrematerial 38 different from metal fibres. As mentioned above, thebushings 7, the metal fibres 13 and the second fibre material 38 areembedded in the polymer matrix of the fibre-reinforced compositematerial of the root region. Preferably, the layers of the second fibrematerial 38 are made of glass and/or carbon fibres.

FIG. 8 shows a sixth embodiment of an elongated bushing 7 provided withmetal fibres 13. The metal fibres 13 are arranged in separate layers 205of metal fibres 13, said layers being in form of fibre bundles, fibremats or fibre strips. A first end of the fibres bundles, mats or stripsis firmly fixed to the second end 10 of the bushing 7. Between layers205 of metal fibres 13, a layer 206 of a second fibre material differentfrom metal is arranged. The layers 205 of metal fibres and the layer 206of a second fibre material are embedded in the polymer matrix of thefibre-reinforced composite material of the root region.

The metal fibres, filaments or wire may have a cross-sectional dimensionin the range between 0.04 mm and 1.0 mm, or in the range between 0.07 mmand 0.75 mm, or in the range between 0.1 mm and 0.5 mm. In some of theembodiments of the longitudinal fastening members, such as the bushing7, the metal fibres may be formed into fibre mats, strips or bundleswhich may be unidirectional mats, strips or bundles, multidirectionalmats, strips or bundles, woven mats or strips, or mats or stripscomprising chopped fibres. Additionally, the metal fibres, filaments orwires may be incorporated into mats, strips or bundles comprising adifferent type of fibres than metal fibres, such as carbon fibres and/orglass fibres, i.e. the metal fibres may be incorporated into so-calledhybrid mats, strips or bundles.

The percentage by volume of metal fibres in the mats, strips or bundlesmay be 20, 30, 40, 50, 60, 70, 80 90 or 100, the remaining fibres beinga different type of fibres, preferably glass and/or carbon fibres.Correspondingly, the percentage by volume of metal fibres in the rootregion, where metal fibres are provided, may be 20, 30, 40, 50, 60, 70,80 90 or 100, the remaining fibres being a different type of fibres,preferably glass and/or carbon fibres.

The embodiment of the embedding element 1 ² according to the inventionshown in FIGS. 10 and 11 is elongated and has a first end 3 ² and anopposite second end 4 ², a first longitudinal lateral face 5 ² and anopposite second longitudinal lateral face 6. Further, the embeddingelement has an upper face 7 ² and a lower face 8 ² interconnecting thelongitudinal lateral face 5 ², 6 ². The first longitudinal lateral face5 ² extends substantially convexly in a cross-sectional view of theembedding element and the second longitudinal lateral face 6 ² extendssubstantially correspondingly concavely in a cross-sectional view of theembedding element 1 ². The upper face 7 ² and the lower face 8 ² areessentially parallel at least over about half the length thereof. Over aremaining portion 22 ² of the length of the upper face 7 ², the uppersurface taper gradually towards the lower face 8 ² so as to form a wedgeshaped embedding element 1 ².

The embedding element 1 ² is formed of a fibre-reinforced compositematerial 9 ² comprising fibres embedded in a polymer matrix. The fibresmay be glass fibres and/or carbon fibre and/or metal fibres, such aspreferably steel or iron fibres and the polymer matrix may be a resinsuch a polyester, epoxy or vinylester.

In the fibre-reinforced composite material 9 ² of the embedding element1 ², an elongated fastening element 10 ² is embedded. The elongatedfastening element 10 ² has an outer surface 11 ², a first end 12 ² andan opposite second end 13 ². Additionally, the elongated fasteningelement 10 ² is provided with an inner longitudinal bore 14 ² extendingfrom the first end 12 ² thereof and being provided with an inner thread15 ².

In the embodiment shown in FIGS. 10 and 11, the elongated fasteningelement 10 ² has a substantially circular cylindrical shape, the outersurface 11 ² thereof being however corrugated.

The elongated fastening element 10 ² is provided with metal fibres 16 ²,preferably formed by iron or steel. A first end 17 ² of the metal fibres16 ² is firmly fixed to the second end 13 ² of the fastening element 1 ²and a portion 18 ² extends essentially axially outwardly from saidsecond end and ends in a second end 19 ² of the metal fibres 16 ².

As described below with reference to FIGS. 12 and 13, the embeddingelement 1 ² may be manufactured by pultrusion in a pultrusion system 40². Pairs 20 ², 20 ²′ of fastening elements are formed by connectingopposite ends of metal fibres 16 ² to second ends 13 ², 13 ²′ of twofastening elements 10 ², 10 ²′ facing each other as shown in FIG. 13.Further, a rod 21 ² of preferably a fibre-reinforced polymer may withits opposite ends be fastened to the second ends 13 ², 13 ²′ of thefastening elements 10 ², 10 ²′ facing each other. Thereby, the pairs 20², 20 ²′ of fastening elements have at least a certain ridigity.Thereafter pairs 20 ², 20 ²′ of fastening elements are mutuallyconnected by means of threaded rods 30 ² preferably made of plasticthreaded into the inner thread 15 ² in the inner longitudinal bore 14 ²in the first ends 12 ², 12 ²′ of juxtaposed pairs of fastening elements10 ², 10 ²′, whereby a string 37 ² of fastening elements has beenformed.

The string 37 ² of fastening elements is as illustrated in FIG. 13introduced into the pultrusion system 40 ², comprising a receivingsection 41 together with webs or bundles of fibre-reinforced materialssuch as webs or bundles of glass fibres and/or carbon fibres and/ormetal/fibres. The webs or bundles of fibres are designated with thereference number 42 ² and 43 ². From the receiving section 41 ² a string44 ² comprising the string 37 ² of fastening elements and the fibre websor bundles 42 ², 43 ² is introduced into a resin applicator and resinheating and curing apparatus 45 ² with a resin reservoir 46 ² to supplyresin thereto. The string 44 ² that has been saturated with resin in theresin applicator and resin heating and curing apparatus 45 ² leaves saidapparatus through a nozzle 46 ² from which a pultruded string 47 ²extends having a cross-section of the embedding element 1 ² in thenot-tapered portion thereof. The pultruded string 47 ² is extracted fromthe nozzle by means of a pulling device 48 ². On the downstream side ofthe pulling device 48 ², a cutting device 49 ² is arranged. The cuttingdevice 49 ² cuts the pultruded string between to fastening elements 10², i.e. the area where the fastening elements 10 ², 10 ²′ are connectedfirst end 10 ² against first end 10 ² by means of the threaded rod 30 ².Thereby, a blank 50 ² comprising two embedding elements 10 ², 10 ²′ isprovided.

FIG. 12 illustrates how this blank 50 ² is cut through along an inclinedcutting line 51 ² extending between the upper and lower face thereof.Thereby, two identical embedding elements 10 ², 10 ²′ are provided, thecut along the inclined cutting line 51 ² providing the tapering portion22 ²of the upper face 7 ² of the embedding elements.

As shown in FIG. 14, several embedding elements 1 ² may be arranged inparallel to allow the convex lateral faces 5 ² to engage the concavelateral faces 6 and such that the first ends 3 ² of the embeddingelements 1 ² are placed in a common plane. Due to the concave and convexlateral faces the embedding elements 1 ² may form a curve, such as acircle in a plane perpendicular to the longitudinal axis of theembedding elements 1 ².

FIG. 15 illustrates the root region 26 ², the transition region 28 ² anda portion of the airfoil region 27 ² of a wind turbine blade made of afibre composite material, and wherein embedding elements 1 ² accordingto the invention have been embedded in the root along the circumferencethereof, such as to allow access to the threaded holes 14 ², 15 ² of theembedding elements 1 ² from the root end face 29 ² of the blade root.The embedding element 1 ² has been arranged in the manner disclosed inFIG. 14, wherein the first lateral face of each embedding element engagethe second lateral face of the juxtaposed embedding element. Thefibre-reinforced composite material of the root region, wherein theembedding elements 1 are embedded comprises fibres embedded in a polymermatrix. The fibres are preferably glass and/or carbon and/or metalfibres preferably steel fibres and the polymer may be a resin such aspolyester, epoxy and vinylester.

LIST OF REFERENCE NUMERALS

-   1-   2 Wind turbine blade-   3 Outer surface of root-   4 Inner surface of root-   5 Outer layer-   6 Inner layer-   7 Elongated fastening member (bushing)-   9 First end of fastening member-   10 Second end of fastening member-   11 Outer periphery of fastening member-   11 a Radially outer surface-   11 b Radially inner surface-   11 c First lateral face-   11 d Second lateral face-   12 Central bore-   13 Metal fibres-   16 First layer comprising metal fibres-   17 Wedge-shaped element-   18 First end of element-   19 Second end of element-   22 Fastening means (inner threads)-   23 Hub-   24 Wind turbine-   25 Nacelle-   26 Root region-   27 Airfoil region-   28 Transition region-   29 Root end face-   31 Blade root-   32 Blade tip-   33 Trailing edge-   34 Leading edge-   35 Chord plane-   36 Tower-   37 Second layers-   38 Second fibre material-   39 Insert-   40 First insert part-   41 Second insert part-   42 Lateral face of insert-   43 Lateral face of insert-   201 First fibre end-   202 Second fibre end-   203 Outwardly extending portion of metal fibres-   204 Metal fibre bundle-   205 Separate layer of metal fibres-   206 Layer of a second fibre material-   1 ² Embedding element-   3 ² First end of embedding element-   4 ² Second end of embedding element-   5 ² First longitudinal lateral face-   6 ² Second longitudinal lateral face-   7 ² Upper face-   8 ² Lower face-   9 ² Fibre-reinforced composite material of the embedding element-   10 ² Elongated fastening element-   11 ² Outer surface of elongated fastening element-   12 ², 12 ^(2,) First end of fastening element-   13 ², 13 ^(2,) Second end of fastening element-   14 ² Longitudinal bore-   15 ² Inner thread-   16 ² Metal fibres-   17 ² First end of metal fibres-   18 ² Portion of metal fibres-   19 ² Second end of metal fibres-   20 ² ,20 ^(2,) Pairs of fastening elements-   21 ² Rod-   22 ² Tapering portion of upper face-   30 ² Threaded rod made of plastic-   37 ² String of fastening elements-   40 ² Pultrusion system-   41 ² Receiving section-   42 ² Webs of fibres-   43 ² Bundles of fibres-   44 ² String-   45 ² Resin applicator heating and curing apparatus-   46 ² Nozzle-   47 ² Pultruded string-   48 ² Pulling device-   49 ² Cutting device-   50 ² Blank-   51 ² Inclined cutting line

1. A wind turbine blade for a wind turbine rotor comprising a hub fromwhich the wind turbine blade extends when mounted to the hub, the windturbine blade including a shell structure of a fibre-reinforcedcomposite material comprising fibres embedded in a polymer matrix, thewind turbine blade extending in longitudinal direction and having aprofiled contour including a pressure side and a suction side as well asa leading edge and a trailing edge, said edges defining a chord planetherebetween, when seen in the longitudinal direction the profiledcontour comprising a root region with a root end face, an airfoil regionand optionally a transition region between root region and the airfoilregion, the root region having a ring-shaped cross section with an outersurface and an inner surface, the root region comprising a plurality ofelongated fastening members provided with fastening means and embeddedmutually spaced apart in the fibre-reinforced polymer so as tosubstantially follow a circumference of the root region and allow accessfrom the outside to the fastening means used for mounting the blade tothe hub, the fastening members comprising an outer surface, a first endarranged at the root end face and a second end opposite the first endthereof, characterised in that at least a number, and preferably all, ofthe elongated fastening members are provided with at least one notch inthe periphery thereof, said notch having a notch wall, a first notch endand an opposite second notch end, and that a rod-shaped locking elementpasses through said notch so as to at least substantially engage atleast a portion of the notch wall and so that a first portion of therod-shaped locking element extends beyond the first notch end and asecond portion of the rod-shaped locking element extends beyond thesecond notch end, the rod-shaped locking element being fixedly arrangedand preferably tightly fitting in a circular bore having an axis andextending at least partly through the shell structure of the root regionfrom the inner or outer surface thereof.
 2. A wind turbine bladeaccording to claim 1, wherein the notch wall is partly cylindrical witha cylinder axis being coaxial with the axis of the bore.
 3. A windturbine blade according to claim 1, wherein the rod-shaped lockingelement has a circular cross section corresponding at leastsubstantially to that of the bore.
 4. A wind turbine blade according toclaim 1, wherein the bore is a through-going bore.
 5. A wind turbineblade according to claim 1, wherein the axis of the bore extendssubstantially in radial direction relative to the root region.
 6. A windturbine blade according to claim 1, wherein the notch is placed atdistance from the first end of the elongated fastening members, saiddistance being 50-95% or 60-95% or 70-95% of the length of the elongatedfastening members.
 7. A wind turbine blade according to claim 1, whereinthe fastening members are provided with two notches, a first notch and asecond notch, said notches being arranged substantially opposite eachother, preferably diametrically opposite each other.
 8. A wind turbineblade according to claim 1, wherein the notches of adjacent fasteningmembers are arranged so as to face each other and the bore and therod-shaped locking element are provided in such a way between theadjacent fastening members that the rod-shaped locking element engagesthe notch wall of both notches.
 9. A wind turbine blade according toclaim 1, wherein the notches of all of the fastening members arearranged at the same distance from the first end of the elongatedfastening members.
 10. A wind turbine blade according to claim 1,wherein the fastening members are bushings, preferably having asubstantially uniform cross section in the longitudinal directionthereof, and the fastening means is a thread in a bore of the bushing.11. A wind turbine blade according to claim 10, wherein the at least onenotch is provided so as to intersect the bore of the bushing.
 12. A windturbine blade according to claim 1, wherein the fastening members andthe rod-shaped locking elements are made of metal, preferably steel. 13.A wind turbine blade according to claim 1, wherein metal fibres,preferably steel fibres, are firmly fixed to the fastening members so asto extend therefrom and are embedded in the polymer matrix of thefibre-reinforced composite material of the root region.
 14. Method ofproducing a wind turbine blade according to claim 1, wherein theelongated fastening members are provided with at least one notch beforebeing embedded in the fibre-reinforced composite material of the rootregion, and wherein the bore is drilled through the composite materialof the root region from the inner or outer surface thereof such that itpasses through the notch and at least substantially reveals the notchsurface and subsequently thereto the rod-shaped locking element isfixedly arranged in the bore, preferably tightly fitting herein. 15.Method of producing a wind turbine blade according to claim 1, whereinthe elongated fastening members are embedded in the fibre-reinforcedcomposite material of the root region and wherein the bore is drilledthrough the composite material of the root region from the inner orouter surface thereof such that it intersects the periphery of theelongated fastening member and thereby provides the notch surface, andsubsequently thereto the rod-shaped locking element is fixedly arrangedin the bore, preferably tightly fitting herein.